Mechanical Properties | Metric | English | Comments |
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Tensile Strength, Yield | 1104 MPa @Strain 0.200 % |
160100 psi @Strain 0.200 % |
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ATI Allvac® 6-2-4-6 Titanium Alloy, Heat Treatment: 885°C (1625°F) + Age Data provided by Allvac.Applications: Intermediate-temperature jet engine applications. Blades, discs, spacers, seals. Standard, rotor/premium grades. |
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Tensile Strength, Yield | 1104 MPa @Strain 0.200 % |
160100 psi @Strain 0.200 % |
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ATI Allvac® 718 Nickel Superalloy, Heat Treatment: 982°C (1800°F) + Age Data provided by Allvac.Applications: Jet engine rings, discs, shafts, compressor blades, seals, spacers. Fasteners, nuclear, oil & gas components. |
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Tensile Strength, Yield | 1104 MPa @Strain 0.200 % |
160100 psi @Strain 0.200 % |
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ATI Allvac® 718-OP® UNS N07718 Nickel Superalloy Uses: Turbines and engines, fasteners, sub-surface safety valves, hot extrusion tooling, nuclear reactors.Property values are for samples in the metallurgical condition: 1800°F age.Information prov.. |
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Tensile Strength, Yield | 1104 MPa @Strain 0.200 % |
160100 psi @Strain 0.200 % |
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ATI Allvac® 720 Nickel Superalloy, Heat Treatment: 1093°C (2000°F) + Age Data provided by Allvac.Applications: Wheels, jet engine turbine discs and blades. |
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Tensile Strength, Yield | 1104 MPa @Strain 0.200 % |
160100 psi @Strain 0.200 % |
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ATI Allvac® 38-644 UNS R58640 Titanium Alloy High-strength, metastable beta alloy. Uses: Spring wire, fasteners, torsion bars for aerospace and automotive applications.Property values are for samples in the metallurgical condition: 1600°F ann.. |